Propulsive Efficiency of Ridge/Inlet Configuration

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0015a.svgz" name="7462024.fig.0015a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>First-order upwind algorithm</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0015b.svgz" name="7462024.fig.0015b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Second-order upwind algorithm</td></tr></table>

<div>Effect of discretization scheme on the vortex structure.</div>

International Journal of Aerospace Engineering

fig15

Figure 15

Figure 15: Propulsive Efficiency of Ridge/Inlet Configuration 